TCH.1C-27J-2-27JG
2-22
SYNCRO SHAFT - REMOVAL AND
INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Disconnect electrical power from aircraft (refer to
).
2.Isolate hydraulic power (refer to manual
3.Remove Pilot and Copilot seat (refer to manual
).
4.Open the access panels 213DZ, 213CZ, 213BZ and
213AZ (214AZ, 214BZ and 214CZ).
Recomended Personnel:
PROCEDURE
MECH.
CODE QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
2
60,00
Removal
AFM
2
40,00
Installation
AFM
2
45,00
Follow
Maintenance
AFM
2
60,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 410 (Min.)
Total Time Detention System: 205 (Min.)
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00181 Kit, flight controls rigging
pins
11G001-C052200-801
27-10-15
2-174